Research of the Photoelectric Tracking and Pointing Platform Based on the Servo Control System

Author:

Shanzhong Liu1ORCID,Pengna Han1ORCID

Affiliation:

1. Henan University of Science and Technology

Abstract

To improve the speed and accuracy of the photoelectric tracking and pointing platform stable tracking, we took the three-axis photoelectric tracking platform, of which the coupling among the rings is ignored, as the research object. Considering the effects of various disturbances, the stable tracking double closed-loop servo control system was built for the azimuth, pitch, and roll rings. In the stabilization loop, output-feedback H∞ controller based on linear matrix inequality was designed to reduce the effects of model perturbations and uncertainties and to maintain the stability of the platform’s inertial space. In the tracking loop, the integral-separation proportional integral derivative (PID) controller was designed to achieve fast and accurate tracking. Smith estimated compensation was adopted to compensate the pure lag caused by video tracking. Finally, the double closed-loop servo control system was built to complete the simulation. The simulation results show that the system not only has good robustness under external disturbances, but also completes the attitude tracking quickly and accurately. Besides, the tracking error is |error| < 5∙e-4 rad, which meets the tracking accuracy requirements.

Funder

National Natural Science Foundation of China

Publisher

FapUNIFESP (SciELO)

Subject

Aerospace Engineering

Reference18 articles.

1. Ambrose H, Qu Z, Johnson R (2001) Nonlinear robust control for a passive line-of-sight stabilization system. Proceedings of the 2001 IEEE International Conference on Control Applications (CCA’01) (Cat. No.01CH37204) p. 942-947. https://doi.org/10.1109/CCA.2001.973991

2. Cheng W-Y, Luo L, Liu Z (2015) Based on the Multi-axis Synchronous Sliding Mode Control of Integral Separation PID Algorithm Research. Modular Machine Tool & Automatic Manufacturing Technique 8(8):97-100.

3. Cui L, Huang H (2007) Design and simulation of highly stable and precise tracking-pointing platform. Journal of Beijing University of Aeronautics and Astronautics 33(12):1462-1465.

4. Gu Q-Y, Song J-M (2007) Design of a missile attitude tracking controller based on H∞ robust output feedback. Acta Armamentarii 28(6):682-685.

5. Guo S-X (2016) Robust reliability based optimal design of H∞ control of parametric uncertain systems. Journal of Dynamic Systems, Measurement, and Control 136(2):1-7. https://doi.org/10.1115/1.4025862

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3